US2821445A - Pistons of compression ignition engines - Google Patents
Pistons of compression ignition engines Download PDFInfo
- Publication number
- US2821445A US2821445A US512840A US51284055A US2821445A US 2821445 A US2821445 A US 2821445A US 512840 A US512840 A US 512840A US 51284055 A US51284055 A US 51284055A US 2821445 A US2821445 A US 2821445A
- Authority
- US
- United States
- Prior art keywords
- piston
- gudgeon pin
- compression ignition
- pistons
- ignition engines
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J1/00—Pistons; Trunk pistons; Plungers
- F16J1/10—Connection to driving members
- F16J1/14—Connection to driving members with connecting-rods, i.e. pivotal connections
- F16J1/16—Connection to driving members with connecting-rods, i.e. pivotal connections with gudgeon-pin; Gudgeon-pins
Definitions
- This invention relates to the pistons of compression ignition engines and is particularly concerned with a type of piston construction in which pressure is transmitted from the piston crown to the gudgeon pin by two vertical walls which are straight where they extend across the interior of the piston at the opposite sides of the gudgeon pin bearing in the connecting rod eye, the said walls coming close together as permitted by the length of said hearing.
- the piston may have a full cylindrical or part cylindrical skirt below the gudgeon pin.
- the width of the piston (in the plane of the gudgeon pin axis) where the said walls are situated beneath the piston ring grooves is less than the diameter of the piston at said grooves so that the heat flow paths from the piston crown tend to keep clear of the piston rings.
- the object of the present invention is to provide improved means for facilitating the transmission of heat from the lower portion of the piston surrounding the gudgeon pin and gudgeon pin bearing in the connecting rod to the relatively cool cylinder walls and to the air and oil within the engine.
- I provide web like extensions of the vertical walls before referred to which transmit pressure from the piston crown to the gudgeon pin, such extensions reaching down below the gudgeon pin bearings and merging at opposite sides into the cylindrical portion of the piston skirt below the gudgeon pin.
- Figure 1 is an elevation
- Figure 2 a sectional elevation at right angles to the Figure 1 view
- Figure 3 a sectional plan view on the line 3-3 of Figure 2
- Figure 4 a sectional plan view on the line 44 of Figure 2 showing a piston of a compression ignition engine constructed in one convenient form in accordance with this invention.
- the piston shown is so constructed that the transmission of pressure from the piston crown a to the gudgeon pin b is effected through two straight vertical walls 0 extending across the piston at the opposite sides of the gudgeon pin hearing in the eye of the connecting rod d, the said walls 0 coming as close together as permitted by the length of said bearing.
- Such web-like extensions e may each have a thickness of from one-two hundred and twenty fifth to one fortieth of the outside diameter of the piston and may have a minimum length below the gudgeon pin axis of three tenths of the outside diameter of the piston.
- the webs may taper downwards as shown for convenience in manufacture.
- My improvement by reason of the disposition of the metal in the web-like extensions, secures improved distribution of pressure upon the surface of the piston sliding within and upon the cylinder bore as the angle of the connecting rod changes during the reciprocation of the piston.
- a piston assembly for a compression ignition engine comprising a crown, a skirt, a gudgeon pin intermediate the crown and the skirt, bosses for the gudgeon pin, two vertical walls between the crown and the gudgeon pin with the walls being straight where the same extend across the interior of the piston assembly at the opposite sides of the gudgeon pin bearing with the pressure transmitted from the crown to the gudgeon pin through such vertical walls, said vertical walls being substantially the same width as that of the bosses for the gudgeon pin, and a web-like extension on each vertical wall extending downwardly below the gudgeon pin bosses with such weblike extensions extending across the skirt in parallel straight lines and the terminal ends of the extensions merging with the skirt.
- each extension is of a thickness of from one-two hundred and twenty fifth to one fortieth of the outer diameter of the piston and of a minimum length below the gudgeon pin axis of three tenths of the outer diameter of the piston.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
J. H. s. GARDNER PISTONS OF COMPRESSION IGNITION ENGINES' Fi led June 2, 1955 United States Patent PISTONS OF COMPRESSION IGNITION ENGINES Joseph Hugh Stott Gardner, Patricroft, near Manchester, England, assignor to L. Gardner & Sons Limited, Patricroft, near Manchester, England, a British com- P y Application June 2, 1955, Serial No. 512,840
Claims priority, application Great Britain July 22, 1954 2 Claims. (Cl. 309-) This invention relates to the pistons of compression ignition engines and is particularly concerned with a type of piston construction in which pressure is transmitted from the piston crown to the gudgeon pin by two vertical walls which are straight where they extend across the interior of the piston at the opposite sides of the gudgeon pin bearing in the connecting rod eye, the said walls coming close together as permitted by the length of said hearing. The piston may have a full cylindrical or part cylindrical skirt below the gudgeon pin. The width of the piston (in the plane of the gudgeon pin axis) where the said walls are situated beneath the piston ring grooves is less than the diameter of the piston at said grooves so that the heat flow paths from the piston crown tend to keep clear of the piston rings.
The object of the present invention is to provide improved means for facilitating the transmission of heat from the lower portion of the piston surrounding the gudgeon pin and gudgeon pin bearing in the connecting rod to the relatively cool cylinder walls and to the air and oil within the engine.
In accordance with the present invention, I provide web like extensions of the vertical walls before referred to which transmit pressure from the piston crown to the gudgeon pin, such extensions reaching down below the gudgeon pin bearings and merging at opposite sides into the cylindrical portion of the piston skirt below the gudgeon pin.
Referring to the accompanying explanatory drawings:
Figure 1 is an elevation, Figure 2 a sectional elevation at right angles to the Figure 1 view, Figure 3 a sectional plan view on the line 3-3 of Figure 2 and Figure 4 a sectional plan view on the line 44 of Figure 2 showing a piston of a compression ignition engine constructed in one convenient form in accordance with this invention.
The piston shown is so constructed that the transmission of pressure from the piston crown a to the gudgeon pin b is effected through two straight vertical walls 0 extending across the piston at the opposite sides of the gudgeon pin hearing in the eye of the connecting rod d, the said walls 0 coming as close together as permitted by the length of said bearing.
In accordance with the present invention, there are web like extensions 2 of the vertical walls 0, such extensions e coming below the gudgeon pin bearings and merging at f at their opposite sides into the cylindrical portion g of the piston skirt below the gudgeon pin.
Such web-like extensions e may each have a thickness of from one-two hundred and twenty fifth to one fortieth of the outside diameter of the piston and may have a minimum length below the gudgeon pin axis of three tenths of the outside diameter of the piston. The webs may taper downwards as shown for convenience in manufacture.
My improvement, by reason of the disposition of the metal in the web-like extensions, secures improved distribution of pressure upon the surface of the piston sliding within and upon the cylinder bore as the angle of the connecting rod changes during the reciprocation of the piston.
What I claim is:
1. A piston assembly for a compression ignition engine comprising a crown, a skirt, a gudgeon pin intermediate the crown and the skirt, bosses for the gudgeon pin, two vertical walls between the crown and the gudgeon pin with the walls being straight where the same extend across the interior of the piston assembly at the opposite sides of the gudgeon pin bearing with the pressure transmitted from the crown to the gudgeon pin through such vertical walls, said vertical walls being substantially the same width as that of the bosses for the gudgeon pin, and a web-like extension on each vertical wall extending downwardly below the gudgeon pin bosses with such weblike extensions extending across the skirt in parallel straight lines and the terminal ends of the extensions merging with the skirt.
2. A piston assembly as defined in claim 1 wherein each extension is of a thickness of from one-two hundred and twenty fifth to one fortieth of the outer diameter of the piston and of a minimum length below the gudgeon pin axis of three tenths of the outer diameter of the piston.
References Cited in the file of this patent UNITED STATES PATENTS 1,057,063 Knudson Mar. 25, 1913 1,768,815 Beckmann July 1, 1930 1,768,816 Beckmann July 1, 1930 2,044,854 Long June 23, 1936 2,313,202 Korytko Mar. 9, 1943 FOREIGN PATENTS 428,051 Great Britain May 7, 1935 564,660 Great Britain Oct. 6, 1944 757,673 France Oct. 16, 1933
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2821445X | 1954-07-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2821445A true US2821445A (en) | 1958-01-28 |
Family
ID=10915935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US512840A Expired - Lifetime US2821445A (en) | 1954-07-22 | 1955-06-02 | Pistons of compression ignition engines |
Country Status (1)
Country | Link |
---|---|
US (1) | US2821445A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3943908A (en) * | 1972-11-03 | 1976-03-16 | Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | One piece piston connected to a connecting rod for high speed four-stroke cycle internal combustion engines |
US8215281B1 (en) | 2009-05-07 | 2012-07-10 | Thomas Edwin Holden | Piston assembly |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1057063A (en) * | 1911-11-18 | 1913-03-25 | Hans Knudsen | Internal-combustion engine. |
US1768816A (en) * | 1929-06-07 | 1930-07-01 | Harry J Hater | Piston |
US1768815A (en) * | 1929-06-07 | 1930-07-01 | Harry J Hater | Piston |
FR757673A (en) * | 1932-06-28 | 1933-12-30 | Bosch Robert | Light metal piston |
GB428051A (en) * | 1933-10-07 | 1935-05-07 | John William Howlett | Pistons |
US2044854A (en) * | 1921-01-17 | 1936-06-23 | Security Trust Company | Piston |
US2313202A (en) * | 1938-01-17 | 1943-03-09 | Korytko Charles Emil Stanislas | Piston |
GB564660A (en) * | 1943-05-07 | 1944-10-06 | Gardner & Sons Ltd | Improvements in the pistons of compression ignition oil engines |
-
1955
- 1955-06-02 US US512840A patent/US2821445A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1057063A (en) * | 1911-11-18 | 1913-03-25 | Hans Knudsen | Internal-combustion engine. |
US2044854A (en) * | 1921-01-17 | 1936-06-23 | Security Trust Company | Piston |
US1768816A (en) * | 1929-06-07 | 1930-07-01 | Harry J Hater | Piston |
US1768815A (en) * | 1929-06-07 | 1930-07-01 | Harry J Hater | Piston |
FR757673A (en) * | 1932-06-28 | 1933-12-30 | Bosch Robert | Light metal piston |
GB428051A (en) * | 1933-10-07 | 1935-05-07 | John William Howlett | Pistons |
US2313202A (en) * | 1938-01-17 | 1943-03-09 | Korytko Charles Emil Stanislas | Piston |
GB564660A (en) * | 1943-05-07 | 1944-10-06 | Gardner & Sons Ltd | Improvements in the pistons of compression ignition oil engines |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3943908A (en) * | 1972-11-03 | 1976-03-16 | Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | One piece piston connected to a connecting rod for high speed four-stroke cycle internal combustion engines |
US8215281B1 (en) | 2009-05-07 | 2012-07-10 | Thomas Edwin Holden | Piston assembly |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2742883A (en) | Oil cooled piston structure | |
US2170099A (en) | Engine having diametrically opposed cylinders | |
US4716817A (en) | Piston, particularly for internal combustion engines | |
US2295199A (en) | Piston | |
US2821445A (en) | Pistons of compression ignition engines | |
US2372050A (en) | Piston | |
US1643720A (en) | Connecting-rod structure | |
US2882106A (en) | Piston for internal combustion engines | |
US3505934A (en) | Piston for internal combustion engine | |
US1758444A (en) | Piston | |
US3374776A (en) | Two-stroke internal combustion engine | |
US2720871A (en) | Piston and connecting rod assembly | |
US1709316A (en) | Composite piston | |
US1795353A (en) | Piston | |
US1492397A (en) | Piston for internal-combustion engines | |
US2190207A (en) | Piston | |
US2661253A (en) | Connecting rod end bearing assembly | |
US4534274A (en) | Piston assembly for internal combustion engines | |
US2383836A (en) | Internal-combustion engine | |
US1883637A (en) | Piston for internal combustion engines | |
US2318954A (en) | Internal combustion engine | |
US2308178A (en) | Piston | |
US2100719A (en) | Piston | |
US2408875A (en) | Piston | |
US1357851A (en) | Composite piston |